Coefficient of lift given drag evaluator uses Lift Coefficient = (Gross Weight*Drag Coefficient)/Drag Force to evaluate the Lift Coefficient, Coefficient of lift given drag is a dimensionless quantity that represents the ratio of lift force to drag force, providing a measure of the aerodynamic efficiency of an object or aircraft, typically used in aerospace engineering and aerodynamics research. Lift Coefficient is denoted by CL symbol.
How to evaluate Coefficient of lift given drag using this online evaluator? To use this online evaluator for Coefficient of lift given drag, enter Gross Weight (W0), Drag Coefficient (CD) & Drag Force (FD) and hit the calculate button.